What it approves
Remove main landing gear doors and associated hydraulic system and cover the wheel wells with a fairing.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (5/14) Page 1 of 2
Reissued on July 14, 2017 to supersede the original STC, which has been lost or misplaced.
Number: SA5737SW
Part 3 of the Civil Air Regulations.
Original Product – Type Certificate Number: 3A21 Make: Cessna Model: 210K, 210L, 210M, T210K, T210L, T210M, P210N Description of Type Design Change:
Remove main landing gear doors and associated hydraulic system, and cover the wheel wells with a fairing in accordance with Installation Instructions dated September 12, 1984, or later FAA approved revision.
Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of Application: April 05, 1984 Date Reissued: July 21, 2005; July 14, 2017 Date of Issuance: June 26, 1984 Date Amended: December 19, 1984 Rev. 1
Signature
Title James A. Grigg Manager, Fort Worth Aircraft Certification Office , Southwest Region Sierra Industries, Ltd.
122 Howard Langford Drive Uvalde, TX 78801
FAA Form 8110-2 (5/14) Page 2 of 2
Transfer the ownership of Supplemental Type Certificate Number: SA5737SW
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 7
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 31, 2017 | Reissued, current | Certificate |
| July 21, 2005 | Reissued, earlier issue | Certificate |